Turbine engine nozzle

Details Turbine engine nozzle Turbine engine nozzle

2005-03-29

2005-03-29

Gartenberg, Ehud (Department: 3746)

Fluid sprinkling, spraying, and diffusing

Reaction motor discharge nozzle

With means controlling amount, shape or direction of...

Reexamination Certificate

active

06871797

ABSTRACT:
A convergent/divergent nozzle for a gas turbine engine has a throat portion of non-constant radius of curvature varying from an upstream high value to an intermediate low value and then to a downstream high value.

REFERENCES:
patent: 4440347 (1984-04-01), Madden et al.
patent: 5511376 (1996-04-01), Barcza
patent: 6398129 (2002-06-01), Johnson

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